FIELD: aviation.
SUBSTANCE: invention relates to the field of aviation. The coupling device is a small towed automatic aircraft (2), including a body, a conical niche with a hook (4), aerodynamic surfaces (5) with electric drives, a light signal source (7), a control system, a machine vision system with a rear-view camera (6), information communication channel and power supply. A conical niche with a hook (4) is located in the rear of the body. Aerodynamic surfaces (5) are located on the housing and are configured to control the position of the hitch in the air flow.
EFFECT: increased speed, reliability, simplicity and safety of aircraft docking.
4 cl, 8 dwg
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RU2518877C1 |
